View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58960U 26157.77958095 +.00000000 +00000-0 +28499-3 0 00007
2 58960 39.9876 179.3589 0009494 128.2916 231.8730 14.95214125 07
| Epoch (UTC): | 06 June 2026 18:42:35 |
| Eccentricity: | 0.0009494 |
| inclination: | 39.9876° |
| perigee height: | 575 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 179.3589° |
| argument of perigee: | 128.2916° |
| revolutions per day: | 14.95214125 |
| mean anomaly at epoch: | 231.8730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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